View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 55060U 26145.44369258 +.00000000 +00000-0 +61798-4 0 00003
2 55060 97.9016 208.9086 0013457 53.8020 306.4433 14.77528866 08
| Epoch (UTC): | 25 May 2026 10:38:55 |
| Eccentricity: | 0.0013457 |
| inclination: | 97.9016° |
| perigee height: | 628 km |
| apogee height: | 647 km |
| right ascension of ascending node: | 208.9086° |
| argument of perigee: | 53.8020° |
| revolutions per day: | 14.77528866 |
| mean anomaly at epoch: | 306.4433° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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